TM 55-1510-219-10
limit for full DOWN extension (100%) of the wing flaps is
control airspeed (Vmc) at sea level standard conditions is 89
157 KIAS. If wing flaps are extended above these speeds,
K I A S .
the flaps or their operating mechanisms may be damaged.
5-26.
MAXIMUM DESIGN MANEUVERING SPEED.
5-25. MINIMUM SINGLE-ENGINE CONTROL
AIRSPEED (VMC).
The maximum design maneuvering speed is 173 KIAS.
Chapter 7, Section X describes minimum single-
engine control airspeed. The minimum single-engine
Section VI. MANEUVERING LIMITS
5-27. MANEUVERS.
G's with wing flaps up or a positive load factor of
2.0 G’s, or a negative 1.227 G’s with wing flaps
a. The following maneuvers are prohibited.
down.
1. Spins.
b. Recommended turbulent air penetration airspeed is
173 KIAS.
2. Aerobatics of any kind.
3. Abrupt maneuvers above 173 KIAS.
5-28. BANK AND PITCH LIMITS.
a. Bank limits are 60° left or right.
4. Any maneuver which results in a positive load fac-
tor of 3.10 G’s or a negative load factor of 1.227
b. Pitch limits are 30° above or below the horizon.
Change 3 5-8.1
